IP Library › Granted Patent US 12,203,796
Granted Patent B2
US 12,203,796 · App. 17/746,397 · Granted Jan 21, 2025

Fluid level sensing arrays for aircraft

Inventor: Nathaniel Ross Bernklau (Keller, TX)
Assignee: Textron Innovations Inc.
G01F23/2924
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Quick Facts
Patent No.
US 12,203,796
App. No.
17/746,397
Granted
Jan 21, 2025
Kind
B2
Abstract

A fluid level sensing system includes a mounting strip and fluid sensing nodes coupled to the mounting strip. Each fluid sensing node is switchable between a fluid present state and a fluid absent state. Each fluid sensing node includes a prism, a photoemitter and a photoreceptor. The photoemitter and photoreceptor are interposed between the prism and the mounting strip. In the absence of fluid around the prism, the photoreceptor receives greater than a threshold amount of light from the photoemitter internally reflected by the prism to switch the fluid sensing node to the fluid absent state. When the prism is covered in fluid, the photoreceptor receives less than the threshold amount of light from the photoemitter to switch the fluid sensing node to the fluid present state. A processor determines a fluid level based on the fluid detection states of the fluid sensing nodes.

Claims (41)

1. A fluid level sensing system comprising:

a mounting strip defining an internal cavity and an outer surface;

a plurality of fluid sensing nodes coupled to the mounting strip in a collinear arrangement, each fluid sensing node switchable between a plurality of fluid detection states including a fluid present state and a fluid absent state, each fluid sensing node comprising:

a prism;

a photoemitter coupled to the outer surface of the mounting strip such that the photoemitter is interposed between the prism and the mounting strip, the photoemitter configured to emit light into the prism; and

a photoreceptor coupled to the outer surface of the mounting strip such that the photoreceptor is interposed between the prism and the mounting strip, the photoreceptor receiving greater than a threshold amount of light from the photoemitter internally reflected by the prism in the absence of fluid around the prism to switch the fluid sensing node to the fluid absent state, the photoreceptor receiving less than the threshold amount of light from the photoemitter when the prism is covered in fluid to switch the fluid sensing node to the fluid present state; and

a processor to determine a fluid level based on the fluid detection states of the fluid sensing nodes;

wherein, the photoemitter and the photoreceptor are located outside the internal cavity of the mounting strip; and

wherein, the prism is coupled to the outer surface of the mounting strip via the photoemitter and the photoreceptor.

2. The fluid level sensing system as recited in claim 1 wherein the mounting strip comprises one or more guard rails to protect the fluid sensing nodes.

3. The fluid level sensing system as recited in claim 1 wherein the mounting strip is configured to be severed at a customizable length adapted for a fluid container.

4. The fluid level sensing system as recited in claim 1 further comprising one or more wires in the internal cavity of the mounting strip electrically interconnecting the fluid sensing nodes.

5. The fluid level sensing system as recited in claim 1 wherein the fluid sensing nodes are uniformly spaced along the mounting strip.

6. The fluid level sensing system as recited in claim 1 wherein each fluid sensing node has a position along the mounting strip, the processor determining the fluid level based on the fluid detection states and the positions of the fluid sensing nodes.

7. The fluid level sensing system as recited in claim 1 wherein each of the prisms is a polymeric prism.

8. The fluid level sensing system as recited in claim 1 wherein the photoemitters of the fluid sensing nodes are wired in series.

9. The fluid level sensing system as recited in claim 1 wherein, for each of the fluid sensing nodes, the photoreceptor receives zero light from the photoemitter when the prism is covered in fluid to switch the fluid sensing node to the fluid present state.

10. The fluid level sensing system as recited in claim 1 wherein the fluid level is proportional to a number of fluid sensing nodes in the fluid present state.

11. The fluid level sensing system as recited in claim 1 further comprising a notification module configured to send fluid level data relating to the fluid level.

12. The fluid level sensing system as recited in claim 11 wherein the notification module sends an alert in response to the fluid level being less than a safe fluid level threshold.

13. The fluid level sensing system as recited in claim 1 wherein the photoemitter and the photoreceptor are coupled to a mounting strip-facing side of the prism.

14. The fluid level sensing system as recited in claim 1 wherein the mounting strip comprises a monolithic mounting strip having a front side, a rear side and lateral sides defining the internal cavity, the outer surface comprising the outer surface of the front side of the mounting strip.

15. An aircraft comprising:

a fuselage;

a fluid container having one or more side walls, the fluid container configured to hold a fluid;

a fluid level sensing array comprising:

a mounting strip coupled to an inner surface of the one or more side walls of the fluid container, the mounting strip defining an internal cavity and an outer surface; and

a plurality of fluid sensing nodes coupled to the mounting strip in a collinear arrangement, each fluid sensing node switchable between a plurality of fluid detection states including a fluid present state and a fluid absent state, each fluid sensing node comprising:

a prism;

a photoemitter coupled to the outer surface of the mounting strip such that the photoemitter is interposed between the prism and the mounting strip, the photoemitter configured to emit light into the prism; and

a photoreceptor coupled to the outer surface of the mounting strip such that the photoreceptor is interposed between the prism and the mounting strip, the photoreceptor receiving greater than a threshold amount of light from the photoemitter internally reflected by the prism in the absence of fluid around the prism to switch the fluid sensing node to the fluid absent state, the photoreceptor receiving less than the threshold amount of light from the photoemitter when the prism is covered in fluid to switch the fluid sensing node to the fluid present state; and

a processor to determine a fluid level of the fluid container based on the fluid detection states of the fluid sensing nodes;

wherein, the photoemitter and the photoreceptor are located outside the internal cavity of the mounting strip; and

wherein, the prism is coupled to the outer surface of the mounting strip via the photoemitter and the photoreceptor.

16. The aircraft as recited in claim 15 wherein the fluid container comprises a gearbox housing for a gearbox and the fluid comprises a lubricating fluid.

17. The aircraft as recited in claim 16 wherein the gearbox comprises a main rotor gearbox disposed in the fuselage.

18. The aircraft as recited in claim 15 wherein the fluid container comprises a fuel tank and the fluid comprises fuel.

19. The aircraft as recited in claim 15 wherein the fluid level sensing array comprises a plurality of fluid level sensing arrays coupled to the one or more side walls of the fluid container; and

wherein, the processor determines a fluid level plane of the fluid in the fluid container based on the fluid detection states of the fluid sensing nodes of the plurality of fluid level sensing arrays.

20. The aircraft as recited in claim 19 wherein each fluid level sensing array occupies a position within the fluid container and the fluid sensing nodes each have a position along a respective mounting strip; and

wherein, the processor determines the fluid level plane based on the fluid detection states of the fluid sensing nodes of the plurality of fluid level sensing arrays, the positions of the fluid level sensing arrays and the positions of the fluid sensing nodes.

Assignments (2)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 18, 2022
From: BELL TEXTRON INC.
To: TEXTRON INNOVATIONS INC.
Reel/Frame 059950/0827 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 17, 2022
From: BERNKLAU, NATHANIEL ROSS
To: BELL TEXTRON INC.
Reel/Frame 059934/0035 →
Continuity (1)
Related Publication 20230375391A1 · Nov 23, 2023
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